Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-hq010-il-100000-n5 Airfoil,hq010-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,36.0427 Max Cl/Cd alpha,4 Url,http://airfoiltools.com/polar/csv?polar=xf-hq010-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.500,-0.7909,0.07517,0.07012,-0.0179,1.0000,0.0211 -11.250,-0.8098,0.06888,0.06371,-0.0222,1.0000,0.0210 -11.000,-0.8304,0.06326,0.05793,-0.0250,1.0000,0.0208 -10.750,-0.8493,0.05873,0.05320,-0.0263,1.0000,0.0209 -10.500,-0.8676,0.05487,0.04909,-0.0259,1.0000,0.0210 -10.250,-0.8844,0.05153,0.04550,-0.0239,1.0000,0.0214 -10.000,-0.8878,0.04869,0.04256,-0.0226,1.0000,0.0225 -9.750,-0.8830,0.04700,0.04077,-0.0215,1.0000,0.0240 -9.500,-0.8781,0.04484,0.03838,-0.0203,1.0000,0.0259 -9.250,-0.8730,0.04222,0.03535,-0.0187,1.0000,0.0284 -9.000,-0.8659,0.03904,0.03161,-0.0170,1.0000,0.0300 -8.750,-0.8536,0.03626,0.02835,-0.0156,1.0000,0.0311 -8.500,-0.8387,0.03392,0.02593,-0.0148,1.0000,0.0336 -8.250,-0.8208,0.03233,0.02414,-0.0140,1.0000,0.0361 -8.000,-0.8009,0.03027,0.02178,-0.0130,1.0000,0.0378 -7.750,-0.7795,0.02840,0.01959,-0.0121,1.0000,0.0396 -7.500,-0.7575,0.02680,0.01774,-0.0112,1.0000,0.0414 -7.250,-0.7367,0.02523,0.01609,-0.0104,1.0000,0.0440 -7.000,-0.7160,0.02416,0.01500,-0.0096,1.0000,0.0479 -6.750,-0.6946,0.02308,0.01381,-0.0087,1.0000,0.0520 -6.500,-0.6740,0.02193,0.01255,-0.0076,1.0000,0.0555 -6.250,-0.6544,0.02086,0.01149,-0.0065,1.0000,0.0604 -6.000,-0.6335,0.02002,0.01054,-0.0055,1.0000,0.0678 -5.750,-0.6134,0.01914,0.00963,-0.0045,1.0000,0.0797 -5.500,-0.5936,0.01824,0.00878,-0.0033,1.0000,0.0946 -5.250,-0.5746,0.01731,0.00800,-0.0022,1.0000,0.1175 -5.000,-0.5566,0.01635,0.00742,-0.0009,1.0000,0.1682 -4.750,-0.5378,0.01563,0.00691,0.0003,1.0000,0.2279 -4.500,-0.5205,0.01488,0.00644,0.0017,1.0000,0.2865 -4.250,-0.5049,0.01412,0.00607,0.0035,1.0000,0.3593 -4.000,-0.4891,0.01357,0.00584,0.0055,1.0000,0.4400 -3.750,-0.4739,0.01318,0.00578,0.0078,1.0000,0.5101 -3.500,-0.4488,0.01301,0.00580,0.0082,0.9942,0.5749 -3.250,-0.4152,0.01299,0.00587,0.0073,0.9837,0.6342 -3.000,-0.3817,0.01304,0.00591,0.0064,0.9741,0.6769 -2.750,-0.3452,0.01306,0.00586,0.0048,0.9662,0.7014 -2.500,-0.3104,0.01306,0.00577,0.0035,0.9570,0.7185 -2.250,-0.2762,0.01305,0.00570,0.0023,0.9478,0.7340 -2.000,-0.2406,0.01305,0.00561,0.0009,0.9400,0.7483 -1.750,-0.2091,0.01305,0.00557,0.0003,0.9295,0.7626 -1.500,-0.1776,0.01307,0.00556,-0.0001,0.9192,0.7784 -1.250,-0.1465,0.01310,0.00555,-0.0003,0.9084,0.7956 -1.000,-0.1158,0.01311,0.00554,-0.0003,0.8978,0.8117 -0.750,-0.0872,0.01311,0.00553,-0.0001,0.8865,0.8251 -0.500,-0.0586,0.01312,0.00553,0.0001,0.8762,0.8367 -0.250,-0.0290,0.01311,0.00551,0.0000,0.8671,0.8474 0.000,0.0000,0.01311,0.00549,0.0000,0.8578,0.8578 0.250,0.0290,0.01311,0.00551,0.0000,0.8474,0.8671 0.500,0.0586,0.01312,0.00553,-0.0001,0.8366,0.8762 0.750,0.0872,0.01311,0.00553,0.0001,0.8249,0.8865 1.000,0.1158,0.01311,0.00554,0.0003,0.8117,0.8978 1.250,0.1465,0.01310,0.00555,0.0003,0.7956,0.9084 1.500,0.1776,0.01307,0.00556,0.0001,0.7784,0.9192 1.750,0.2091,0.01305,0.00557,-0.0003,0.7626,0.9295 2.000,0.2406,0.01305,0.00561,-0.0009,0.7483,0.9399 2.250,0.2762,0.01305,0.00570,-0.0023,0.7341,0.9478 2.500,0.3105,0.01306,0.00577,-0.0035,0.7185,0.9570 2.750,0.3452,0.01306,0.00586,-0.0048,0.7014,0.9662 3.000,0.3817,0.01304,0.00590,-0.0064,0.6768,0.9741 3.250,0.4152,0.01299,0.00587,-0.0073,0.6342,0.9837 3.500,0.4488,0.01301,0.00580,-0.0083,0.5751,0.9942 3.750,0.4738,0.01318,0.00578,-0.0078,0.5099,1.0000 4.000,0.4891,0.01357,0.00584,-0.0055,0.4401,1.0000 4.250,0.5049,0.01412,0.00607,-0.0035,0.3599,1.0000 4.500,0.5205,0.01488,0.00644,-0.0018,0.2867,1.0000 4.750,0.5379,0.01563,0.00691,-0.0003,0.2282,1.0000 5.000,0.5566,0.01635,0.00742,0.0009,0.1682,1.0000 5.250,0.5746,0.01731,0.00800,0.0022,0.1173,1.0000 5.500,0.5936,0.01824,0.00878,0.0033,0.0946,1.0000 5.750,0.6134,0.01914,0.00963,0.0045,0.0796,1.0000 6.000,0.6334,0.02003,0.01055,0.0055,0.0676,1.0000 6.250,0.6545,0.02086,0.01148,0.0065,0.0604,1.0000 6.500,0.6739,0.02195,0.01257,0.0076,0.0554,1.0000 6.750,0.6946,0.02308,0.01381,0.0087,0.0520,1.0000 7.000,0.7160,0.02416,0.01500,0.0096,0.0479,1.0000 7.250,0.7366,0.02524,0.01609,0.0104,0.0439,1.0000 7.500,0.7575,0.02680,0.01775,0.0112,0.0414,1.0000 7.750,0.7795,0.02840,0.01959,0.0121,0.0395,1.0000 8.000,0.8008,0.03027,0.02179,0.0130,0.0378,1.0000 8.250,0.8208,0.03233,0.02414,0.0140,0.0361,1.0000 8.500,0.8387,0.03393,0.02594,0.0148,0.0337,1.0000 8.750,0.8536,0.03625,0.02833,0.0156,0.0311,1.0000 9.000,0.8658,0.03906,0.03164,0.0171,0.0300,1.0000 9.250,0.8731,0.04219,0.03532,0.0187,0.0284,1.0000 9.500,0.8778,0.04493,0.03848,0.0203,0.0260,1.0000 9.750,0.8837,0.04685,0.04061,0.0215,0.0239,1.0000 10.000,0.8886,0.04854,0.04239,0.0226,0.0224,1.0000 10.250,0.8843,0.05155,0.04553,0.0239,0.0215,1.0000 10.500,0.8682,0.05496,0.04916,0.0258,0.0211,1.0000 10.750,0.8504,0.05872,0.05317,0.0263,0.0210,1.0000 11.000,0.8307,0.06331,0.05797,0.0250,0.0209,1.0000 11.250,0.8115,0.06868,0.06351,0.0222,0.0210,1.0000 11.500,0.7906,0.07535,0.07029,0.0178,0.0212,1.0000